A method for making a plural-component, composite-material, highway dowel-bar including (1) preparing an elongate core train possessing endo-abutting, longitudinally alternating, (a) elongate, high-shear-strength, cylindrical cores having a common cross section, and (b) elongate, but shorter, cylindrical, fiber-reinforced plastic-resin end-plug blanks having opposite ends, and each having a cross section matching the cross section of the cores, (2) using the core train as a longitudinally moving mandrel, pultrusion-forming a fiber-reinforced plastic-resin sleeve continuously and bondedly around the core train so as to produce a pultrusion-result, intermediate, dowel-bar product, and (3) following pultrusion-forming, cross-cutting the intermediate, dowel-bar product at each longitudinal location therein which is intermediate the opposite ends of the end-plug blanks, thereby to form completed dowel bars.
|
6. A method of manufacturing a composite-material highway dowel-bar, the method comprising:
providing a train of cylindrical steel cores along a long axis, with each adjacent pair of steel cores separated by a single cylindrical blank;
forming a fiber-reinforced plastic-resin sleeve around the train by passing the train through a pultrusion die, thereby forming an intermediate dowel-bar product; and
cutting through the intermediate dowel-bar product to form completed dowel-bars;
wherein cutting through the intermediate dowel-bar product includes cutting through each blank so that a first portion of each blank is included in a first completed dowel-bar and a second portion of each blank is included in a second completed dowel-bar.
1. A plural-component, composite-material, highway dowel-bar making method comprising
preparing an elongate core train having a long axis, and possessing, along that axis, endo-abutting, longitudinally alternating, (a) elongate, cylindrical cores, each core having a common, constant cross section at every location along the long axis, and (b) elongate, but shorter, cylindrical, fibre-reinforced plastic-resin end-plug blanks having opposite ends, and each end-plug blank having a constant cross section at every location along the long axis matching the constant cross section of the cores,
using the core train as a longitudinally moving mandrel, pultrusion-forming a fibre-reinforced plastic-resin sleeve continuously and bondedly around the core train so as to produce a pultrusion-result, intermediate, dowel-bar product, and
following said pultrusion-forming, cross-cutting the intermediate, dowel-bar product at longitudinal locations therein which are intermediate the opposite ends of end-plug blanks, and thereby forming completed dowel bars.
2. The method of
3. The method of
4. The method of
5. The method of
7. The method of
8. The method of
|
This is a divisional application from currently copending U.S. Regular patent application Ser. No. 13/756,507, filed Jan. 31, 2013, for “Plural-Component, Composite-Material Highway Dowel Bar Structure and Fabrication Methodology”, which prior application claims filing-date priority to U.S. Provisional Patent Application Ser. No. 61/595,042, filed Feb. 4, 2012, for “Highway-Slab Dowel Interconnect Structure”. The entire disclosure contents of these two applications are hereby incorporated herein by reference.
This invention relates to methodology focused on making a unique, plural-component, composite-material highway (especially concrete-highway) dowel bar structure having features which successfully address, and resolve, key, serious, and interrelated, functional-reliability, componentry cost, and highway lifecycle economic problem issues that have for years been associated with highway dowel-bar technology, and relationally, with certain aspects of highway functionality longevity.
The architecture of this methodology is described herein in a manner intentionally intertwined with a companion description of the unique dowel bar which is fabricated in accordance with it.
Dowel bars are ubiquitous in concrete highway construction. They take the form of elongate, cylindrical, high-shear-strength, smooth-exterior rods, typically formed of conventional, structural steel (non-stainless), which are employed in multiple numbers, typically at 1-foot lateral-spacing intervals, as shear-bridging, slab-to-slab load-transfer components at each separation interface (joint) which exists between adjacent, travel-direction-oriented, highway slabs that are usually formed of poured concrete, and preferably, in many instances, of what is known in the art as high-performance concrete. Their most important functions are to furnish appropriate bad-transfer shear strength between adjacent slabs while at the same time (a) accommodating slab expansion and contraction (with slight, but recurrent, slab-joint openings and closings) due to ambient thermal changes, and additionally (b) minimizing the phenomenon known as slab faulting at the joints between adjacent slabs. They are conceived as simple structures, sometimes differently formed, in relation to efforts to achieve improvements over the use alone of conventional structural steel, of materials, and combinations of materials, such as epoxy-coated structural steel, zinc-coated structural steel, solely stainless steel, stainless-steel-jacketed conventional structural steel, and purely single-unit plastic composite materials—all intended to perform the above-mentioned, important “highway-performance-support” functions flawlessly for long periods of time.
However, for a number of costly and disappointing reasons outlined below, they do not do this. Intent and reality historically have not matched successfully, and the resulting hunt for necessary, important, and fundamental dowel-bar improvement, has for years been, and is still, ongoing.
It is our belief that a dowel bar which is made in accordance with the practice/methodology features of the present invention changes this situation, and that the “hunt” just mentioned may now be substantially over.
Further regarding aspects of the background, dowel-bar setting which has triggered the conception and reduction to practice of the present methodology invention, dowel bars are employed in the multi-millions in concrete highway construction, both in the United States and in numerous other countries. In such highway construction, the usual, adjacent highway-pavement slabs that lie, edge-to-edge, along a normally constructed highway lane may typically have a length of about 15-feet, and a width of about 12-feet. Between each, successive, adjacent lane slab, dowel bars, at about 1-foot lateral intervals, are included as interconnecting structures.
Because of what are currently very predictable, current-dowel-bar-materials' wear and corrosion characteristics, and due to the facts (1) that dowel bars, and the confronting, concrete faces of their associated highway slabs, are both exposable at all inter-slab, concrete highway joints, and (2) that dowel bars, during their operative lives, are subjected to substantial cyclic shear loads in the multi-millions even over relatively short periods of time—a condition which is very relevant to the durabilities and configurations of the intended, protective coatings that are furnished for various types of coated steel bars (mentioned below), they are not, and cannot comfortably be considered to be, permanent, or even satisfactorily and relatively long-lasting components of concrete highway structure in many applications. A result is the need for too-frequent dowel-bar (and associated concrete-slab) replacement—an extraordinarily costly need.
Despite many improvement-focused efforts launched in the past to minimize the necessity for, and the attendant frequencies of, highway dowel-bar replacement, these efforts have not been entirely successful. For example, and considering commonly understood corrosion and wear issues that are associated with known dowel-bar constructions, typical, widely-used, conventional steel dowel bars are obviously subjected to environmental-conditions rusting and corrosion, and do not possess characteristics which inherently help to resist these issues. Among past “improvement” attempts, purely stainless steel dowel bars, while less vulnerable, though not immune, to corrosion, nevertheless are eventually corrodible, and, very significantly, are extremely expensive as items, per se, and often prohibitively so.
Other improvement fabrication approaches taken in the past, such as coating traditional structural steel dowel bars with, for example, thin layers of epoxy or zinc, is expensive, and, for a variety of reasons, has not worked particularly well. Apart from the expense issue, and considering specifically structural matters, epoxy coatings are typically applied by spraying (or by some other suitable, surface-application technique) to long “over-lengths” of conventional, structural-steel, dowel-bar core material, with the resulting, long, core-coated product then crosscut selectively to achieve finished dowel bars of the desired lengths. The crosscut, end areas are usually then simply left uncoated, with the result that exposed steel exists at those cut ends which are thus fully exposed to all nearby, corrosive environmental conditions.
Where epoxy coating is applied completely over already pre-length-cut steel dowel-bar cores, i.e., where no post-coating cross-cutting is involved, or under those circumstances where cross-cut ends are in fact subsequently coated with epoxy, the resulting all-over epoxy coating effectively “flows” extends as a material-continuum over the sharp-edged surface discontinuities that exist, at each end of a dowel bar, between the cylindrical surface of the core steel bar material and the end surfaces of this material—a condition which thus exposes the coating material, at these sharp discontinuity regions, to very high-stress mechanical conditions, with respect to which cyclic loading of dowel bars, in their installed use conditions in concrete highway slabs, easily triggers regional stress fractures in a coating—fractures which then expose the core steel material at those vulnerable locations to corrosion-attack environmental conditions.
Another main concern involving epoxy-coated steel bars is that typical rough handling and installation of these bars damages (i.e., cracks, chips, etc.) and noticeably compromises the protective effectiveness of the employed epoxy material.
Zinc coating of conventional structural steel bar material produces dowel bars that also present a problematic issue. Zinc coating is employed as a corrosion-accepting, sacrificial layer over steel, inhibiting steel corrosion, yes, but in its sacrificial role becoming extremely roughly surface-textured, a condition interfering with the desired capability of a dowel bar to offer smooth-outside-surface sliding contact with surrounding concrete to accommodate necessary, temperature related expansion and contraction of concrete slabs.
Solid, fibre-reinforced, plastic-based, composite-material dowel bars have been proposed and tried, but, as individuals, they do not offer the shear strength of steel, and thus do not function well as comparably robust, slab-to-slab load transferors. Accordingly, where such plastic, reinforced dowel bars are selected for use, they are usually employed (a) in greater numbers, and (b) with closer lateral spacings, than are characteristic for steel dowel bars, and at least for this reason involve greater expense. Stainless-steel-jacketed, conventional steel dowel bars are quite expensive, and notwithstanding stainless jacketing, in some instances, disappointingly, also corrodible.
With these negative, expense and corrosion-driven, performance-longevity matters in mind, one of the most significant issues involving extensive dowel-bar use in concrete highway construction is that, when dowel-bar replacement becomes necessary—and frequently too often so—the materials and labor-time and -wage costs, and the related downtime associated with the need for construction-site-preparation and the subsequent pouring of new highway concrete slab material (because of the fact that, where failed dowel bars are located, the surrounding concrete highway material must be demolitioned), are extraordinary.
In this setting, there is clearly a need for an improved highway dowel bar which offers, along with impressive-performance shear strength, great resistance to corrosion decay, with both of these qualities and characteristics collaboratively contributing to (1) significant reduction of replacement need, (2) appreciable lengthening of replacement intervals where replacements are required, and in the bargain, (3), impressive minimizing of highway lifecycle, etc. costs. These considerations, while important in all concrete highway settings, are particularly important considerations where a highway is to be what is known as a high-performance highway built with high-performance/long-life concrete.
Accordingly, fabricated by practice of the methodology of the present invention is a plural-component, composite-material highway dowel bar including an elongate, high-shear-strength, cylindrical core, preferably, although not necessarily, formed of steel, and an elongate, fibre-reinforced plastic-resin jacket fully surrounding and protectively covering the entirety of the core, and exposed to no high-stress-point discontinuities, such as surface-edge discontinuities, anywhere within the overall dowel-bar structure. The jacket includes, as it results from practice of the associated invention methodology, an elongate, fiber-reinforced, cylindrically tubular, plastic-resin sleeve which circumsurrounds and is bonded to the core. The jacket sleeve, which is intentionally made longer than the inside steel core, has opposite ends that extend beyond the associated opposite ends of the received core, thus to define, together with the inwardly disposed core ends, a pair of spaced, single-open-ended, elongate, cylindrical, sleeve end wells, or simply end wells. Two, elongate, cylindrical, fiber-reinforced, plastic-resin sleeve end plugs (also referred to herein simply as plugs), each having a diameter and a cross section matching that of the steel core, fill the sleeve end wells, and are united in the overall dowel-bar structure by a bonding mechanism, such as one or more of those mentioned immediately below, which firmly secures them to the sleeve in the end wells. These plugs, together with the receiving sleeve, protectively seal the side and opposite ends of the core. The central, high-shear-strength core and the two end plugs in each dowel bar are collectively referred to as a core assembly. The outside of the sleeve is smooth. Tenacious bonding between the sleeve and the inside core assembly may include any one or more of several bonding mechanisms, including sleeve shrinkage, normal mill scale roughness of steel, associated, of course, just with the steel core, molecular inter-material forces with both the steel core and the end plugs, and other.
Thus, and very importantly, nothing about the protective jacket, and its making in accordance with the present invention, involves any condition of jacket-material “folding” around and over the sharp edge discontinuities that are present adjacent the ends of the central steel core. This important condition exists chiefly because of the fact that the sleeve in the jacket is formed, pursuant to practice of the present invention, with a length which is greater than that of the steel core, that the sleeve extends beyond each of the opposite ends of the core, and that sleeve-received and bonded end plugs having diameters and cross sections matching that of the core close the opposite ends of the sleeve to complete the core-protective jacket.
The jacket's included sleeve is fibre reinforced in plural, resin-embedded, fibre-differentiated, circumferentially-adjacent circumferential layers of fibres which take the forms of (1) elongate, linear, plural-elongate-fibre-including, glass-fibre roving material whose included fibres substantially parallel the long axis of the dowel bar, (2) continuous-glass-fibre mat material, and (3), glass-fibre veil material. The sleeve end plugs are formed preferably of roving-fibre-reinforced plastic resin, wherein the included fibres are linear and also disposed substantially parallel the long axis of the dowel bar.
The methodology of the invention proposes a pultrusion-based, dowel-bar making process including, in general terms, (a) preparing an elongate core train (preferably substantially horizontally disposed) possessing endo-abutting, longitudinally alternating (1) elongate, cylindrical, high-shear-strength cores, and (2) shorter, elongate, cylindrical and matching-cross-section resin and fiber-reinforced, pre-pultruded sleeve end-plug blanks, (b) using the core train as a longitudinally moving mandrel, pultrusion-forming a resin and fiber-reinforced sleeve continuously and bondedly around the core train so as to produce a pultrusion-result intermediate product, and (c) cross-cutting the pultrusion-result intermediate product at the longitudinal center locations of the sleeve end plugs to form the final dowel bars.
Pre-pultrusion, of the just-above-mentioned, pre-pultruded sleeve end plugs does not specifically, or necessarily, form a methodologic, procedural part of the present invention, and may be conducted in an entirely conventional manner. Such pre-pultrusion, however, is a very useful end-plug-making technique for assuring that the end plugs, in order to cooperate successfully in the dowel bar made by practice of the invention, are satisfactorily reinforced with throughout-distributed, elongate, linear fibres that substantially parallel the end plugs' long axes.
These and other features and advantages of, and offered by, the methodology of the invention will become more fully apparent as the detailed description of it which follows below is read in conjunction with the accompanying drawings.
Components, structures and positional relationships between elements presented in
Turning now to the drawings, and referring first of all to
Focusing especially on
The principal components present in bar 10 include (1) an elongate, cylindrical, high-shear-strength core 12, preferably, though not necessarily, made of steel, having a long axis 12a which is coincident with axis 10a, and spaced, opposite ends 12b, (2) an elongate, pultrusion-formed, fiber-reinforced plastic-resin jacket 14 having an elongate, pultrusion-formed, cylindrically tubular sleeve 16 which, within its elongate, hollow, cylindrical interior, or inside, 16a, snugly and circumsurroundingly receives core 12, and (3) a pair of pre-pultrusion-formed, cylindrical, sleeve end plugs 18 which, disposed immediately next to core 12's ends 12b, as seen, are adhesively/bondedly received complementarily within the cylindrical, opposite ends, or end wells, 16b of sleeve 16 to close off the ends of this sleeve. Sleeve 16 includes a long axis 16c which is coincident with axes 10a, 12a, and a circumferential wall 16d. Plugs 18, together with sleeve 16, form the entirety of jacket 14 which completely surrounds and sealingly protects steel core 12.
While different dimensions designed to suit different particular applications are of course entirely possible throughout the structure of the dowel bar fabricated in accordance with the present invention, dowel bar 10 herein has a fairly typical set of outer dimensions, with a length (D1 in
Conventional structural steel is employed for core 12, and a particular steel which is very suitable is known as Grade ASTM 615-60 carbon steel.
Within jacket 14, three, different, or differentiated, characters of plastic-resin-embedded, reinforcing fibers, preferably made of glass, and most preferably of e-glass, are employed. These differentiated fibre characters include (1) glass-fibre roving, also referred to herein as elongate, linear, plural-elongate-fibre-including, glass-fibre roving material whose included fibres substantially parallel previously mentioned axes 10a, 12a, 16c, (2) glass-fibre mat, also referred to as continuous-glass-fibre mat material, and (3) glass-fibre veil, or veil material. All three of these characters of fibres are employed in sleeve 16 in what are referred to as circumferentially-adjacent, fibre-differentiated, radially spaced, circumferential (effectively cylindrically tubular) layers that are disposed circumferentially around the long axis 16c of the sleeve, within its wall 16d. Solely the roving material is employed in cylindrical end plugs 18, the fibres in which material are distributed across each plug's entire, circular cross section, with the linear fibres in such roving material substantially paralleling axes 10a, 12a and 16c.
While the reinforcing fibers employed are most preferably made of e-glass, we recognize that they might alternatively be made, for other examples, of s-glass, basalt, or carbon.
Each type of the just-mentioned, three fibre-reinforcing materials is conventional, is offered commercially in a wide variety of choices, particular sizes and other characteristics, and may freely be selected for use successfully in the making of the dowel bar being described, with such selecting being made according to specific highway applications and designer-choice considerations. Representatively, fibre-reinforcing materials which we have found to be well-suited for use in many high-performance highways include: (a), for mat material, continuous-strand glass fibre products made and offered by Owens Corning in Pennsylvania, USA; (b), for roving material, a selection drawn from the products also made by Owens Corning; and (c), for veil material, what are referred to respectively as “tissue veil” and “veil cloth” products made available by Freudenberg Nonwovens in Durham, N.C., and Xamax in Seymour, Conn.
The embedding, plastic-resin material preferably used with the reinforcing fibres in the sleeve is a conventional, urethane-modified, thermoset, vinylester resin material, such as Dion 31038-00, made by Reichhold Inc. in Durham, N.C., USA. In the end plugs, we have chosen, as a preferred plastic resin material, a conventional, thermoset polyester material, made by Razor Composites in Baraboo, Wis.
As was mentioned in relation to what is illustrated in
Language which commonly describes both of these embodiments, in relation to the structure of sleeve 16, is that this sleeve, which is, as already mentioned, elongate and cylindrically tubular, is pultrusion formed, in accordance with practice of the present invention, of fiber-reinforced plastic resin, and specifically is formed with plural, plastic-resin-embedded, fiber-differentiated, circumferentially-adjacent circumferential (generally cylindrical and tubular-like) layers of fibers which are preferably glass fibers, and specifically, most preferably c-glass fibers, as mentioned above. In one dowel-bar and sleeve embodiment, referred to below as a first, or first-mentioned, dowel bar and sleeve embodiment, chooseable for employment in many, high-performance highway applications, there are three, circumferential layers of structurally differentiated fibers, and in the other dowel-bar and sleeve embodiment, referred to below as a second, or second-mentioned, dowel-bar and sleeve embodiment, selectable for use in many, other, high-performance highway applications, there are four such layers. Accordingly, in
In both dowel bar embodiments described herein, the glass material present in sleeve 16 occupies about 60% by weight of the sleeve.
Layer 20, which appears as a wavy line in
Discussing this illustrated, overall layer organization in what may be thought of as a “one-removed-layer” manner that relates specifically to the above-mentioned sleeve embodiment which features only three fibre-reinforcing layers, one sees in sleeve 16, i.e., in its wall 16d, by appropriately visualizing
Alternatively, by looking at
The pre-pultruded sleeve end plugs, as mentioned earlier herein, include elongate roving fibers distributed across the entireties of the plugs′ circular cross sections, embedded in the mentioned, thermoset, polyester resin present in the sleeve. These fibres extend substantially parallel to axes 10a, 12a and 16c.
Returning here for a moment to the very important topic mentioned above involving the fact that jacket 14, as distinguished from known, prior-art, core-component, over-coating structures, is not subjected to contact with any sharp-edged, high-stress, surface discontinuity regions within the dowel bar constructed as described herein, it is easy to see and understand, from the descriptions and illustrations which have now been presented of the sleeve and end-plug components which make up jacket 14, that no part of this jacket structure bears upon the sharp-edged surface discontinuity regions that exist adjacent the opposite ends of core 12, as can be seen at the two, such, regional locations in
Turning attention now in succession to
Progressing from left to right, i.e., from upstream to downstream ends of apparatus 28, across
It should be understood that, while four, fibre-delivery spools (devices) have been illustrated in
Further discussing what has just been described respecting
Located preferably adjacent both (1) the upstream, or infeed, and (2) the downstream, or discharge, ends of apparatus 28, are suitable track-like, such as trough-like, and preferably, though not necessarily, stationary, support structures, not illustrated herein, that provide appropriate, underlying support (a), adjacent the upstream end of the apparatus for what will shortly be described as a stream of elements that make up a pre-pultrusion core-train of dowel-bar central elements (i.e., endo-abutting, longitudinally alternating cores and end-plug blanks) that are to be fed into die 48 for pultrusion forming of sleeve structure 16, (b), adjacent the downstream end of the apparatus, and of die 48, for the emerging intermediate, pultrusion-result, dowel-bar product, such as that shown at 54, and (c), beyond cross-cutter 52, for the finished and thereafter separated dowel bars 10. Other modes, etc., of underlying “component-throughput-transport” support may, of course, be implemented.
While the process of sleeve formation herein is clearly a pultrusion-based process, at the extreme upstream end of apparatus, there are engaged herein, as will now be described, upstream, core-train-forming and core-train-pushing, operational stages that relate to the needed formation, and then the downstream-transport-moving, of what has been described, referred to above, as a core train of components that become organized into a horizontal, linear train in any suitable, component-placement manner in station 34 for feeding from that station toward stations 45, 46, and pultrusion die 48. As mentioned earlier herein, what is referred to as a core train, such as the one pictured fragmentarily, and horizontally, at 56 in
Considering now the overall dowel-bar formation pultrusion process proposed by the present invention, a core train, including endo-abutting, longitudinally alternating cores and end-plug blanks, is suitably formed along a line in forming station 34. Within this station, as the formed core train is moved by pusher 32 toward the pultrusion die, and by appropriately timed and staged operation of previously described heater H1, which may take any suitable form of a heater selected by the user, and which may conveniently and conventionally be operated under the control of a suitably programmed, digital computer (not part of the present invention), the steel cores in the train are preferably heated, as mentioned earner herein, to a temperature of about 150° F. Such heating is preferably done in order to prevent the cores, during processing within pultrusion die 48, from acting as undesired heat sinks which could retard, and perhaps interfere with, appropriate curing of the resin which coats the fiber reinforcing materials within the die.
The formed core train, with its included, appropriately pre-pultrusion-activity, heated, steel cores, is moved from the forming station toward and into the die by pusher 32, which is operated in any appropriate fashion, entirely selectable by the user, to shift the core-train components at an appropriate rate toward and into the pultrusion die, and in a manner so as to accommodate, as far as the pultrusion die is “concerned”, a substantially steady and effectively continuous stream of freshly die-introduced core-train components.
There are many conventional ways that a pusher, such as schematically illustrated pusher 32, may be constructed and operated so as (1) to permit easy, essentially continuous assembly in station 34 of a progressively formed core-train line of components, and (2), at appropriate moments to push these train-formed components in proper, endo-abutting conditions so that the pultrusion die will experience a continuity inflow of dowel-bar, core-component material. Those skilled in the art will recognize that once the substantially “endless” core train, pushed to an appropriate location along pultrusion-formation axis 28a, is sufficiently disposed within the pultrusion die, and specifically sufficiently contained therewithin so that resin-coated, fibre reinforcing, sleeve material has begun to stick to the core train, the downstream operation of puller 50 “takes over” in conventional pultrusion fashion, and functions, in a continuity manner to drive the downstream-directed, flowing motion of all within the die.
It should be noted here that proper endo abutment between the cores and end-plug blanks in a core train, during the core-train forming process, and the associated moving of a formed core train into die 48, depends upon the opposite ends of the cores and end-plug blanks lying correctly in parallel planes that are disposed normal to the respective long axes of these components.
While these core-train forming and pushing activities are underway in apparatus 28 in station 34 and by pusher 32, elongate runs, such as those, previously mentioned, shown at 20, 22, 24, 26 in
If the first-discussed dowel-bar embodiment is to be made, fibre-material paying out takes place from spools 20, 22, 26, whereas if the second-discussed embodiment is to be formed, such paying out occurs from all four, illustrated spools.
Within pultrusion die 48, as the through-moving core train, and the associated, surrounding, wetted-fiber-reinforced, materials pass through the die, an appropriate level of heat, generated inside the die (at the previously mentioned, representative, internal temperature of about 280° F.) by heater H2, coupled with the attendant, moving-surface-contact which occurs with the internal, cylindrical pultrusion channel within the die, cause the resin-coated mass of material to form appropriately around the core train in the configuration of what is to become a sleeve 16. The plastic resin material cures effectively to doneness by the time that all of these materials emerge from the downstream end of the die. Curing of the plastic resin material within die 48 is, of course, promoted by heat which is generated by heater H2, and to some extent by heat radiated from the pre-heated steel cores which, because of their pre-heated conditions, do not negatively act as unwanted heat sinks within the die.
It will be well understood by those skilled in the art that (1) the rate of throughput of materials established selectively in apparatus 28 in the formation of dowel bars, (2) the selected level of internal-die heating which is created by heater H2, and (3) the overall length of die 48, per se, are appropriately determined by the specifically chosen sizes of the materials that are to be employed in the making of a particular size and character of a dowel bar 10, and in relation to the formation curing characteristics of the chosen plastic resin material.
As has been mentioned herein, what emerges continuously during dowel-bar-making, from the downstream, discharge end of die 48, is what has been referred to hereinabove as an intermediate, pultrusion-result, dowel-bar product, as seen at 54 in
Downstream from die 48, and under appropriate operational and timing control, such as might be implemented by a suitably programmed digital computer, cross-cutter 52 is operated to produce a cross cut in this emerging “intermediate” product, with each such cut being made at a location which is substantially exactly midway between the opposite ends of each core-plug blank. Such a cross cut is shown generally at 59 in
The result of this operation is, of course, separation, one after another, of completed dowel bars 10 made in accordance with the invention.
Outlining now compactly, in relation to the block/schematic diagram presented in
(a) preparing an elongate core train having a long axis, and possessing, along that axis, endo-abutting, longitudinally alternating, (1) elongate, high-shear-strength, cylindrical cores having a common, certain cross section, and (2) elongate, but shorter, cylindrical, fibre-reinforced plastic-resin end-plug blanks having opposite ends, and each having a cross section matching the certain cross section of the cores—Block 60,
(b) using the core train as a longitudinally moving mandrel, pultrusion-forming a fibre-reinforced plastic-resin sleeve continuously and bondedly around the core train so as to produce a pultrusion-result, intermediate, dowel-bar product—Block 64, and
following pultrusion-forming, cross-cutting the intermediate, dowel-bar product at each longitudinal location therein which is intermediate the opposite ends of the end-plug blanks, and thereby forming completed dowel bars—Block 66.
From an augmented point of view, this methodology further contemplates that pultrusion-forming is preceded by (a) paying out, from suitable supplies, continuous, elongate runs of reinforcing fibre materials, (b) bathing these materials runs in curable, liquid plastic resin, and guiding the bathed runs into circumferential layer structure for pultrusion in a tubular region circumsurroundingly disposed relative to the outside of the prepared core train—Block 62.
Other features of this methodology are discussed above, and include employing, as reinforcing fibre materials, (1) glass-fibre roving possessing plural, elongate, linear fibres, (2) continuous-glass-fibre mat, and (3), glass-fibre veil, and the paying out and guiding steps collaboratively perform arranging of the different reinforcing fibre materials whereby, relative to the outside surface of the core train during the pultrusion-sleeve-forming step, mat material becomes disposed as part of an innermost pultrusion layer, veil material becomes disposed as part of an outermost pultrusion layer, and roving material becomes part of a layer which is intermediate these innermost and outermost layers, with its included, elongate fibers disposed with their long axes substantially paralleling the core train's long axis.
Accordingly, the present invention features a special pultrusion-based fabrication methodology, in certain variations for creating a pair of modifications of important, new, advanced-performance and significantly-enhanced-longevity highway dowel bars. Variations and modifications are, of course, possible which will come within the spirit of the invention, and which may well come to the minds of those generally skilled in the relevant art.
Gibson, Robert C., Noble, Matthew H., Garber, Trent J.
Patent | Priority | Assignee | Title |
10508390, | Feb 04 2012 | Composite Rebar Technologies, Inc. | Plural-component, composite-material highway dowel bar fabrication methodology |
10858789, | Sep 20 2016 | COMPOSITE REBAR TECHNOLOGIES, INC | Hollow, composite dowel bar assemblies, associated fabrication methodology, and apparatus |
Patent | Priority | Assignee | Title |
3283050, | |||
4265981, | May 17 1977 | COMMONWEALTH SCIENTIFIC AND INDUSTRIAL RESEARCH ORGANIZATION, A BODY CORPORATE | Impact-resisting composites |
4296060, | Dec 07 1979 | PPG Industries Ohio, Inc | Method of producing a pultruded, fiber reinforced rod |
4780166, | Jun 26 1987 | Shell Oil Company | Method and apparatus for producing elongated articles from fiber-reinforced plastic material |
4814133, | Jul 24 1986 | Ube-Nitto Kasei Co., Ltd. | Method of forming the spacer of an optical fiber cable |
5055324, | Nov 08 1988 | REICHHOLD, INC ; SURFACE TECHNOLOGIES, INC | Method of forming a synthetic surface simulating stone, marble or the like |
5084221, | Dec 28 1988 | Ube-Nitto Kasei Co., Ltd. | Process for manufacturing a twisted FRP structure |
5166230, | Sep 16 1991 | REICHHOLD, INC | Method for producing a synthetic shaped article simulating marble, granite or the like |
5182064, | Oct 17 1990 | Nippon Oil Company, Limited | Method for producing fiber reinforced plastic rods having helical ribs |
5567374, | Nov 01 1991 | Applied Research of Australia, Pty. Ltd. | Polymeric moldings reinforced with tows of fibers |
5593536, | Jun 28 1994 | Marshall Industries Composites | Apparatus for forming reinforcing structural rebar |
5593744, | Dec 06 1993 | Oregon Reinforcement Engineering, Ltd. | Hollow reinforcing members and composites containing the same |
5609806, | Jun 28 1994 | Reichhold Chemicals, Inc. | Method of making prepreg |
5626700, | Jun 06 1995 | Marshall Industries Composites | Method for forming reinforcing structural rebar by pultruding a core and molding thereover |
5650109, | Jun 28 1994 | Reichhold Chemicals, Inc.; Marshall Industries Composites | Method of making reinforcing structural rebar |
5702816, | Jun 28 1994 | MARSHALL COMPOSITE TECHNOLOGIES, LLC | Reinforcing structural rebar and method of making the same |
5729952, | Dec 11 1995 | Mechanical rebar couplers | |
5763042, | Jun 28 1994 | MARSHALL COMPOSITE TECHNOLOGIES, LLC | Reinforcing structural rebar and method of making the same |
5851468, | Jun 28 1994 | MARSHALL COMPOSITE TECHNOLOGIES, LLC | Reinforcing structural rebar and method of making the same |
5876553, | Jun 28 1994 | MARSHALL COMPOSITE TECHNOLOGIES, LLC | Apparatus for forming reinforcing structural rebar |
5904886, | Jul 21 1995 | Surface Technologies | Process for making a multi-layered decorative article |
5950393, | Jul 27 1998 | Surface Technologies, Inc. | Non-corrosive reinforcing member having bendable flanges |
5966895, | Jul 27 1998 | Surface Technologies, Inc. | Non-corrosive reinforcing member having bendable flanges |
6023903, | Jul 27 1998 | Surface Technologies, Inc. | Non-corrosive reinforcing member having bendable flanges |
6092960, | Oct 27 1997 | RJD INDUSTRIES, LLC | Concrete joint restraint system |
6171016, | Oct 20 1998 | CONCRETE SYSTEMS, INC | Tubular reinforcing dowel system and method |
6197395, | Dec 06 1993 | OREGON REINFORCEMENT ENGINEERING, LTD | Hollow reinforcing members and composites containing the same |
6221295, | Oct 07 1996 | MARSHALL INDUSTRIES COMPOSITES, INC | Reinforced composite product and apparatus and method for producing same |
6316074, | Oct 07 1996 | MARSHALL INDUSTRIES COMPOSITES, INC | Reinforced composite product and apparatus and method for producing same |
6403004, | Jul 21 1995 | Surface Technologies, Inc. | Process for making a multi-layered solid surface article |
6485660, | Oct 07 1996 | MARSHALL COMPOSITE TECHNOLOGIES, LLC | Reinforced composite product and apparatus and method for producing same |
6493914, | Oct 07 1996 | MARSHALL COMPOSITE TECHNOLOGIES, LLC | Reinforced composite product and apparatus and method for producing same |
6517277, | Sep 22 1998 | Kansas State University Research Foundation | Expansion and crack joint coupler |
7553554, | May 27 2004 | ARTAZN LLC | Environmentally protected reinforcement dowel pins and method of making |
7632037, | Aug 05 2004 | CONSTRUCTION MATERIALS, INC | Dowel apparatus and method |
8206059, | Sep 14 2011 | Load transfer assembly | |
8413396, | Aug 11 2009 | Wisconsin Alumni Research Foundation | Splice system for connecting rebars in concrete assemblies |
20050123374, | |||
20050232697, | |||
20080261042, | |||
20080318042, | |||
20100031607, | |||
20120066994, | |||
20130202355, | |||
AU729030, | |||
CN2832896, | |||
DE2500375, |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Jan 30 2013 | NOBLE, MATTHEW H | COMPOSITE REBAR TECHNOLOGIES, INC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 031255 | /0164 | |
Jan 30 2013 | GARBER, TRENT J | COMPOSITE REBAR TECHNOLOGIES, INC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 031255 | /0164 | |
Jan 31 2013 | GIBSON, ROBERT C | COMPOSITE REBAR TECHNOLOGIES, INC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 031255 | /0164 | |
Sep 21 2013 | Composite Rebar Technologies, Inc. | (assignment on the face of the patent) | / |
Date | Maintenance Fee Events |
May 04 2020 | REM: Maintenance Fee Reminder Mailed. |
Sep 14 2020 | M2551: Payment of Maintenance Fee, 4th Yr, Small Entity. |
Sep 14 2020 | M2554: Surcharge for late Payment, Small Entity. |
May 06 2024 | REM: Maintenance Fee Reminder Mailed. |
Date | Maintenance Schedule |
Sep 13 2019 | 4 years fee payment window open |
Mar 13 2020 | 6 months grace period start (w surcharge) |
Sep 13 2020 | patent expiry (for year 4) |
Sep 13 2022 | 2 years to revive unintentionally abandoned end. (for year 4) |
Sep 13 2023 | 8 years fee payment window open |
Mar 13 2024 | 6 months grace period start (w surcharge) |
Sep 13 2024 | patent expiry (for year 8) |
Sep 13 2026 | 2 years to revive unintentionally abandoned end. (for year 8) |
Sep 13 2027 | 12 years fee payment window open |
Mar 13 2028 | 6 months grace period start (w surcharge) |
Sep 13 2028 | patent expiry (for year 12) |
Sep 13 2030 | 2 years to revive unintentionally abandoned end. (for year 12) |